Method of manufacturing a face plate for a golf club head

Abstract

golf club heads with patterned face plates described herein. Other examples, embodiments and related methods are also disclosed herein.

Description

CROSS-REFERENCE TO RELATED APPLICATIONS

This application is a continuation of U.S. patent application Ser. No. 11/854,998, filed on Sep. 13, 2007, which is a division of U.S. patent application Ser. No. 10/803,837 filed on Mar. 17, 2004, now U.S. Pat. No. 7,347,794. The contents of the disclosures listed above are incorporated herein by reference.

BACKGROUND

This invention relates generally to golf clubs and, in particular, to so-called metal wood drivers.

Recent developments in golf club design have included improvements in drivers, which are clubs used primarily to strike a golf ball resting on a golf tee. These improvements have resulted in drivers with club heads consisting of a hollow shell usually made of metal, such as steel, aluminum, or titanium. These hollow shells have relatively thin walls including a thin front wall that is used to impact the golf ball. In order to prevent the front wall of these hollow shells from permanently deforming or cracking upon ball impact, it has become necessary to reinforce the front wall. One example of a golf club head consisting of a hollow metal shell with a reinforced front wall is disclosed in U.S. Pat. No. 4,511,145 to Schmidt. The club head disclosed in the Schmidt patent has an arched ridge extending between the heel and toe ends of the front wall. The arched ridge design of the Schmidt provides adequate reinforcement for drivers of moderate head volume, however, in an effort to obtain better and better performance from these hollow metal wood drivers, golf club manufacturers have increased the head volume from the moderate volume of 200 cc's to over 400 cc's during the past decade. As head size increases, less and less material is available to reinforce the front wall of the club face within acceptable weight limitations (i.e., around 200 grams mass). Consequently, more exotic materials such as forged or cold rolled titanium faces welded to a cast titanium body have been utilized in these super-oversized drivers. The rear surfaces of the front walls of these super-oversized drivers must be carefully contoured to provide adequate structural strength with a minimum amount of material.

The most critical region to reinforce, is, of course, the ideal ball impact point of the front wall. Because most golfer's swings vary somewhat from impact to impact, the reinforced region of the front wall must be distributed around the ideal impact point. However, since variations in a golfer's swing tend to be more in the heel and toe direction, rather than up or down, the distribution of hits tends to be within a horizontal, elliptical region rather than a circular region centered around the center of the club face. Accordingly, an elliptical, rather than a purely circular reinforcement is preferable. One example of a golf club head having a face with a contoured rear surface is U.S. Pat. No. 6,354,962 to Galloway, et al. The club head disclosed in Galloway has a face plate reinforced with elliptical regions that are formed as part of the forging process of the face plate. For clubs in which the club face is machined from a wrought alloy sheet or other sheet material, forming an elliptical reinforced region presents special problems. The face cannot be machined properly on a lathe because the lathe will produce only a circular reinforced region. One manufacturer is known to use an end mill that makes multiple elliptical passes to machine the reinforced region of the golf club face. This operation is, however, time consuming and unnecessarily costly.

SUMMARY

According to the present invention, a golf club head is manufactured by removing a portion of the rear surface of a face plate to form a central thickened region surrounded by a transition region that tapers to a thinner peripheral region. According to the illustrative embodiment, the face plate is a rolled sheet titanium alloy between 0.130 and 0.180 inches thick, a portion of the transition region of which is machined away to leave the central thickened region and to form the transition region and the thinner peripheral region. Rather than forming the rear surface contour of the face plate by making multiple passes with an end mill, however, the central portion, the transition region and the peripheral region are formed in a single elliptical pass with a special cutting tool. The cutting tool, or “form cutter” has a conical lateral cutting surface, which forms the transition region and the peripheral region in a single operation. Use of this form cutter to machine the transition region and peripheral region in a single operation yields greater uniformity in the rear surface contour of the face plate and saves substantial time and money over prior art multiple pass machining operations.

BRIEF DESCRIPTION OF THE DRAWING

The present invention will be better understood from a reading of the following detailed description, taken in conjunction with the accompanying drawing figures in which like references designate like elements, and in which:

FIG. 1 is a partially cut-away rear perspective view of a golf club incorporating features of the present invention;

FIG. 2 is a rear cross-sectional view of the golf club of FIG. 1;

FIG. 3 is a cross-sectional view of the golf club of FIG. 2 taken along line 3-3;

FIG. 4 is a cross-sectional view of the golf club of FIG. 2 taken along line 4-4;

FIG. 5 is a side view of a machining step in the method of forming golf club head in FIG. 2;

FIG. 6 is a side view of an alternative cutting tool used in the machining step of FIG. 5; and

FIG. 7 is a side view of another alternative cutting tool used in the machining step of FIG. 5.

DETAILED DESCRIPTION

The drawing figures are intended to illustrate the general manner of construction and are not necessarily to scale. In the description and the in the drawing figures, specific illustrative examples are shown and herein described in detail. It should be understood, however, that the drawing figures and detailed description are not intended to limit the invention to the particular form disclosed but are merely illustrative and intended to teach one of ordinary skill how to make and/or use the invention claimed herein and for setting forth the best mode for carrying out the invention.

Referring to FIG. 1, a golf club 10 includes a head 12, a hosel 14 and a shaft 16. Head 12 includes a hollow body 18 made of a metal material such as titanium. Hollow body 18 is formed as a shell 20, which may be assembled from a series of forged pieces but, in the illustrative embodiment, comprises a titanium investment casting. A face plate 22 is attached by conventional means such as plasma or electron beam welding to a corresponding opening 23 in shell 20 to form hollow body 18. Face plate 22 may be a conventional forged blank but, in the illustrative embodiment, comprises a rolled sheet titanium blank that is machined prior to welding to shell 20 as described more fully hereinafter.

As noted hereinbefore, because a golfer's swing tends to vary more in the heel-toe direction than it does up or down, the inventor of the present invention determined that the most efficient reinforcement would be an elliptical thickened region oriented so that the major axis of the reinforced region was substantially horizontal when the club is held in its normal position for addressing the ball. Accordingly, face plate 22 includes a central thickened region 24 that is substantially elliptical in shape with its major axis 26 oriented horizontal when the club is held in its normal address position. In the illustrative embodiment, central thickened region 24 is between 0.130 and 0.180 inches in thickness. Central thickened region 24 is surrounded by a transition region 28 that tapers from the central thickened region 24 to a peripheral region 30, which in the illustrative embodiment is 0.080 to 0.120 inches thick. Transition region 28 is also elliptical, however, for reasons that are explained more fully hereinafter, the major axis and minor axis of transition region 28 are a fixed amount larger than the respective major and minor axis of central thickened region 24. Accordingly, the aspect ratio of transition region 28 is lower than the aspect ratio of central thickened region 24 (in other words, transition region 28 is a “fatter” ellipse than central thickened region 24).

With reference to FIGS. 2-5, prior to assembly of face plate 22 to shell 20, the rear contours of face plate 20 are formed by a machining operation shown schematically in FIG. 5. The process begins with a blank face plate 32, which in the illustrative embodiment comprises a blank stamped from a rolled sheet of titanium alloy. The blank face plate 32 has a thickness equal to the final thickness of the central thickened region 24 of the finished face plate 22, which as noted hereinbefore is from 0.130 to 0.180 inches in thickness. The rear surface of blank face plate 32 is machined by using a cutting tool 34 to remove a portion thereof. The tip of cutting tool 34 has a lateral cutting surface 36 and a lower cutting surface 38. Lower cutting surface 38 is perpendicular to the axis 40 of cutting tool 34. Lateral cutting surface 36 is angled upward with respect to lower cutting surface 38 by an angle 42 of from about 5 to 20 degrees, but preferably about 13 degrees such that lateral cutting surface 36 defines a generally inverted conical frustum surface of revolution 44 as cutting tool 34 is rotated about its axis 40. Lateral cutting surface 36 may have straight edges as shown in FIG. 5, or may have edges 36b that are concave downward as in the cutting tool 34b shown in FIG. 6, or may have edges 36c that are convex downward as in the cutting tool 34c shown in FIG. 7. yielding a conical frustum surface of revolution (and corresponding transition regions) having correspondingly curved sides.

As can be seen from FIG. 5, as the lower cutting surface 38 and lateral cutting surface 36 are brought into contact with rear surface 46 of blank face plate 32, lower cutting surface 38 and lateral cutting surface 36 cooperate to cut a tapered transition region 28 and a flat perimeter region 30 simultaneously in a single pass, thus obviating the need to make multiple passes with an end mill as in the prior art. With particular reference to FIGS. 2-4, the major axis 26 of central thickened region 24 is from 0.65 to 1.05 inches in length. The minor axis 48 of central thickened region 24 is 0.25 to 0.45 inches in length. Accordingly, the aspect ratio of central thickened region 24 is between 1.4 and 4.2. In the illustrative embodiment, major axis 26 is approximately 0.85 inches and minor axis 48 is approximately 0.35 inches yielding an aspect ratio of approximately 2.4.

Major axis 50 and minor axis 52 of transition region 28 are a fixed amount “δ” greater than the respective major and minor axes of central thickened region 24, wherein the δ value can be chosen from a range of about 0.40 inches to about 1.20 inches. In the illustrative example, the major axis 50 and minor axis 52 are approximately 0.86 inches greater than the respective major and minor axes of central thickened region 24. Thus, major axis 50 in the illustrative embodiment is approximately 1.71 inches in length and minor axis 52 of transition region 28 is approximately 1.21 inches in length. Thus, the aspect ratio of transition region 28 is approximately 1.4 as opposed to the 2.4 aspect ratio of central thickened region 24. The high aspect ratio central raised portion surrounded by the lower aspect ratio transition region provides optimum distribution of material for improved performance and reliability.

As the rules to golf may change from time to time (e.g., new regulations may be adopted or old rules may be eliminated or modified by golf standard organizations and/or governing bodies such as the United States Golf Association (USGA), the Royal and Ancient Golf Club of St. Andrews (R&A), etc.), golf equipment related to the apparatus, methods, and/or articles of manufacture described herein may be conforming or non-conforming to the rules of golf at any particular time. Accordingly, golf equipment related to the apparatus, methods, and/or articles of manufacture described herein may be advertised, offered for sale, and/or sold as conforming or non-conforming golf equipment. The apparatus, methods, and/or articles of manufacture described herein are not limited in this regard.

While at least some of the above examples have been depicted and/or described with respect to one or more types of golf clubs, the apparatus, methods, and/or articles of manufacture described herein may be applicable to other types of golf clubs. In some examples, the apparatus, methods, and/or articles of manufacture describe herein may be applicable to driver-type golf club(s), fairway wood-type golf club(s), hybrid-type golf club(s), iron-type golf club(s), wedge-type golf club(s), and/or putter-type golf club(s). Alternatively, the apparatus, methods, and/or articles of manufacture described herein may be applicable other type of sports equipment such as hockey stick(s), tennis racket(s), fishing pole(s), ski pole(s), etc.

Although certain illustrative embodiments and methods have been disclosed herein, it will be apparent from the foregoing disclosure to those skilled in the art that variations and modifications of such embodiments and methods may be made without departing from the spirit and scope of the invention. Accordingly, it is intended that the invention should be limited only to extent required by the appended claims and the rules and principals of applicable law.

Claims

1. A method for manufacturing a golf club head comprising:

providing a face plate material for a face plate having a strike side and a back side; and milling the face plate material in an elliptical pattern to concurrently form, in a single elliptical orbit:

a central region comprising a first elliptical outer edge;

a transition region extending from the first elliptical outer edge to a second elliptical outer edge; and

a peripheral region bounding the transition region and extending from the second elliptical outer edge out to a face plate edge of the face plate; wherein:

the elliptical pattern and the first, second, and face plate edges are non-circular;

the transition region comprises a substantially constant width throughout the transition region and between the first and second elliptical outer edges; and

from the strike side to the back side of the face plate material:

an entirety of the central region within the first elliptical outer edge is thicker than the transition region past the first elliptical outer edge and thicker than the peripheral region past the second elliptical outer edge.

2. The method of claim 1, wherein:

the elliptical pattern, and the first, and second elliptical outer edges, have a contour different than a contour of the face plate edge.

3. The method of claim 1, wherein:

milling the face plate further comprises:

milling the face plate material in the single elliptical orbit such that no further passes are required to complete the milling of the face plate material to define the central region, the transition region, and the peripheral region.

4. The method of claim 1, wherein:

milling the face plate material comprises:

using a form cutter to mill the face plate material, the form cutter comprising first and second cutting surfaces different from each other;

wherein:

the second cutting surface is substantially flat and perpendicular to a rotating axis of the form cutter;

the transition region is formed by the first cutting surface during the single elliptical orbit;

the second cutting surface extends from the second edge to the face plate edge such that the peripheral region is formed by the second cutting surface during the single elliptical orbit; and

the form cutter does not contact the central region, except for the first elliptical outer edge, during the single elliptical orbit.

5. The method of claim 4, wherein:

each point along the second elliptical outer edge is displaced outward from the first elliptical outer edge by a first predetermined distance determined by the first cutting surface.

6. The method of claim 1, wherein:

the transition region comprises a non-linear transition from the first elliptical outer edge to the second elliptical outer edge; and

an entirety of the non-linear transition of the transition region is convex relative to the strike side.

7. The method of claim 1, wherein:

the transition region comprises a non-linear transition from the first elliptical outer edge to the second elliptical outer edge; and

an entirety of the non-linear transition of the transition region is concave relative to the strike side.

8. The method of claim 1, wherein:

a centerpoint of the central region comprises a thickness substantially similar to a blank face plate thickness of the face plate material.